Steam Turbine Startup Bypass Loop for Rapid Pressure Admission

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Solution Overview

Problem

Traditional combined cycle power systems face inefficiencies and high emissions during startup due to low load holds and gas turbine loading rate restrictions, leading to increased starting and loading time, fuel consumption, and air emissions.

Innovation Solution

A main steam startup control bypass loop with a main steam bypass stop valve and control valve is introduced to allow for rapid steam turbine startup, decoupling the gas turbine from the steam turbine, enabling high-efficiency, low-pressure-drop steam control and reduced emissions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If traditional low load holds and gas turbine loading rate restrictions are applied during startup, then steam temperature can be controlled to match steam turbine bowl metal temperature, but air emissions increase and starting and loading time increases

Engineering Contradiction:
Improvesteam temperature matchingVSAvoidstarting and loading time
Core Design Contradiction:
TemperatureVSLoss of time

Solution Approach 1:

The steam control system is segmented into multiple independent control paths: a bypass control valve for rapid steam admission during startup, and a main control valve for normal operation. This segmentation allows the bypass valve to handle the critical startup phase with fast response, while the main valve manages steady-state operation, thereby reducing startup time without compromising temperature matching capability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A bypass control valve is introduced as an intermediary component between the steam source and the steam turbine. This intermediary valve provides a dedicated rapid-response pathway for steam admission during startup, decoupling the startup control function from the main control valve and enabling faster response times while the main valve continues to provide stable control during normal operation.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Temperature

If traditional low load holds are applied during startup, then steam temperature can be controlled, but fuel consumption increases due to gas turbine operating at low efficiency

Engineering Contradiction:
Improvesteam temperature controlVSAvoidfuel consumption
Core Design Contradiction:
TemperatureVSUse of energy by moving object

Solution Approach 1:

The control system is divided into bypass control valve for startup phase and main control valve for normal operation. This allows the gas turbine to operate at optimal load levels during startup since the bypass valve can rapidly admit steam without requiring the turbine to be held at low load, thereby improving fuel efficiency while maintaining temperature control.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bypass control valve serves as an intermediary that enables rapid steam admission during startup, eliminating the need to hold the gas turbine at inefficient low load levels. This intermediary mechanism decouples the temperature control function from the gas turbine loading rate, allowing the turbine to operate at higher efficiency while the bypass valve manages the steam temperature matching during startup.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Temperature

If traditional low load holds are applied during startup, then steam temperature can be controlled, but air emissions increase

Engineering Contradiction:
Improvesteam temperature controlVSAvoidair emissions
Core Design Contradiction:
TemperatureVSObject-generated harmful factors

Solution Approach 1:

By segmenting the steam control into bypass and main valves, the system eliminates low-load holding during startup. The bypass valve enables rapid steam admission that allows the gas turbine to operate at higher load levels from the start, avoiding the high emissions associated with low-efficiency operation at low load while maintaining precise steam temperature control.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bypass control valve acts as an intermediary that enables fast steam admission during startup, allowing the gas turbine to skip the high-emission low-load phase. This intermediary mechanism provides a direct pathway for steam control that decouples temperature management from gas turbine loading restrictions, thereby reducing emissions while achieving temperature matching.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Speed

If main steam control valve is used for rapid startup, then steam admission can be controlled, but the valve experiences severe throttling duty and reliability issues

Engineering Contradiction:
Improvestartup speedVSAvoidvalve reliability
Core Design Contradiction:
SpeedVSReliability

Solution Approach 1:

The valve system is segmented into two specialized valves: a bypass control valve optimized for rapid startup with linear flow characteristics and minimal throttling, and a main control valve optimized for steady-state operation. This segmentation allows the bypass valve to handle the severe startup conditions without compromising reliability, while the main valve handles normal operation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bypass control valve serves as an intermediary component specifically designed to handle the severe throttling duties during rapid startup. This intermediary valve protects the main control valve from excessive wear and reliability issues by isolating it from the most demanding startup conditions, while still enabling fast startup performance through the bypass pathway.

Inventive Principle:
Principle #24Intermediary (Mediator)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution enables faster gas turbine startup with reduced emissions and increased revenue by enhancing steam turbine control fidelity and minimizing rotor stresses, while maintaining low pressure drop and rapid closure for turbine protection.

Implementation Method 1

The bypass loop control facilitates combined cycle startup with full pressure steam turbine admission

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Implementation Method 2

The bypass loop includes a bypass control valve, which may be modulated during startup and loading

Methodology Applied
Scientific EffectFluid flow control:

Data Source

PatentUS8176723B2Apparatus for starting a steam turbine against rated pressure
Publication Date: 2012.05.15 GE INFRASTRUCTURE TECH LLC
  • US8176723B2 patent drawing
  • US8176723B2 patent drawing
  • US8176723B2 patent drawing

AI summary

An external steam turbine main steam startup control valve bypass loop is provided to facilitate a full pressure combined cycle rapid response/fast start powerplant. The main steam startup bypass control loop particularly includes a main steam startup bypass control valve, which allows for the implementation of high efficiency, low pressure drop main steam control valve that otherwise would not be able to handle the severe throttling duty during a full pressure steam turbine startup and enhances the controllability of the steam turbine allowing for the high fidelity controls necessary to minimize steam turbine rotor stresses.